Appendix B
Euler‐Bernoulli Beam Equation

The readers are referred to Adhikari and Bhattacharya (2010), Bhattacharya and Adhikari (2011), and Arany et al. (2015a,b, 2016, 2017) for comprehensive understanding. The fundamentals are provided here.

The equation of motion using the Euler‐Bernoulli beam model for a beam with an axial force is

B.1equation

where EI(z) is the bending stiffness distribution along the axial coordinate z, μ(z) is the distribution of mass per unit length, P* is the axial force acting on the beam due to the top head mass and the self‐weight of the tower, p(z, t) is the excitation of the beam, w(z, t) is the deflection profile.

Using constant equivalent values for the axial force, bending stiffness and mass per length, and considering free harmonic vibration of the beam with separation of variables w(z, t) = W(z) · eiωt, the equation can be reduced to the following using the non‐dimensional parameters of Table B.1 and the dimensionless axial coordinate ξ = z/L:

B.2equation

Table B.1 Nondimensional variables.

Dimensionless group Formula Dimensionless group Formula
Nondimensional lateral stiffness images Nondimensional axial force images
Nondimensional rotational stiffness images Mass ratio images
Nondimensional cross stiffness images Nondimensional rotary inertia images

KL, KR, KLR are the lateral, rotational, and cross stiffness of the foundation, respectively; EIη is the equivalent bending stiffness of the tapered tower; LT is the hub height above the bottom of the tower; P* is the modified axial force, mRNA is the mass of the rotor‐nacelle assembly; mT is the mass of the tower; J is the rotary inertia of the top mass; μ is the equivalent mass per unit length of the tower.

where images is the nondimensional axial force and images is the non‐dimensional circular frequency).

Using the nondimensional numbers as defined above, the boundary conditions can be written for the bottom of the tower (ξ = 0):

B.3equation
B.4equation

and the top of the tower (ξ = 1):

B.5equation
B.6equation

The parameters used in the boundary conditions are defined in Table B.1. The characteristic equation for the equation of motion can be written as

B.7equation

and

equation

The four solutions are then

B.8equation

with which the solution is in the form

B.9equation

which can be transformed using Euler's identity to

B.10equation

with

B.11equation

Substituting this form of the solution into the boundary conditions, one obtains four equations, written in matrix form as

B.12equation

with

B.13equation

and

equation
B.14equation

Looking for nontrivial solutions of this equation one obtains

B.15equation

from which one can obtain the nondimensional circular frequency Ω, and from that the natural frequency using

B.16equation

The equation that has to be solved is transcendental and therefore solutions can only be obtained numerically.

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